Search

17 results found
HOPAS (Hybrid online policy adaptations strategy) on OPS-SAT

While AI technologies have shown promise in various applications in the space industry, their adoption on spacecraft flight software has yet to happen in a significant manner. This is due to a number of factors, including the relatively low computing power available on board of traditional spacecrafts, the long development process required in the industry and the lack of opportunities for in-orbit demonstrations. Airbus teams have identified in ESA OPS-SAT a unique opportunity to quickly test promising algorithms in-orbit as it seeks to resolve the issues listed above.

United Kingdom

21-D-S-OPS-02-a

Airbus Defence &...
Star Tracker Based Generic Safe Mode for Science Missions

A previous study (TRP Star sensing based safe mode) confirmed the interest of using star tracker as primary sensor in a generic safe mode: versatility, suitability to complex requirements and constraints (e.g.

France

T205-119SA

AIRBUS DEFENCE AND SPACE...
Mars Surface Platform Capabilities Study

The Mars Surface Platform Capabilities Study aimed to provide ESA with an assessment of the state of the art in Mars lander technologies using ESA/European technologies with flight heritage. Airbus’ Mars lander experience is taken from the Beagle 2 probe launched in 2003 on board Mars Express.

The objectives of the study were to:

UK

20-P-M-HRE-01-b

Airbus Defence &...
Securing NG-Ultra FPGA development through innovative System-on-a-Chip (SoC) validation
The BRAVE series of reprogrammable FPGA’s represent an entirely new area of development for microelectronics. These high performance, very advanced electronics could revolutionise the manufacturing process and performance of multiple missions. Alongside their development there is a current industry initiative to standardise avionics systems. As part of this venture, GSTP Element 2 has initiated an activity to develop a standardised box, which will contain all the different computer modules, such as power boards, and ensure they are all compatible.
France

GT27-046ED

AIRBUS DEFENCE AND SPACE...
Impact of controlled and semi-controlled re-entry on Spacecraft design

There is increased attention being given to safeguarding Earth's orbital environment, as reflected by the number of relevant regulations that are being set forward by national governments and international organisations. Among others, ESA has published a Space Debris Mitigation Policy for Agency Projects (ESA/ADMIN/IPOL(2014)2), supported by the corresponding ESA Space Debris Mitigation Compliance Verification Guidelines (ESSB-HB-U-002).

UK

15/718

Airbus Defence &...
High-Altitude pseudo-satellites for telecommunication and complementary space applications

The interest in HAPS is increasing in many areas, from military and security to commercial services. On the telecommunications side, HAPS are seen as relays to provide internet services worldwide, and as a possible complement to satellites. On the Earth observation side, the near-space location of the HAPS enables new services or could improve the existing satellite ones. From the satellite or from the HAPS market sides, it is important to understand how both systems can offer complementary services, and what the possible synergies between them are.

France

15/708-b

Airbus Defence &...
End of Life operations for disposal of mega‐constellations

The objective of this activity was to understand the operational complexity of large mega-constellation systems, and the potential needs to operate these, including the complexity of collision avoidance manoeuvres (CAMs). This objective was achieved by:

Germany

15/052

Airbus Defence &...
Feasibility of ultra low thrust transfers in L1, L2, Sun, Earth & Moon Systems

A set of tools has been developed to enable assessment of the feasibility of ultra-low thrust transfers in regions of multi-body gravity field influence. Aspects include:

France

15/723-a

Airbus Defence &...
GEROS-ISS Cost Reduction Exercise

The main goal of GEROS-ISS is to demonstrate the capabilities of GNSS remote sensing to derive geophysical parameters of ocean, ice and land surfaces, which are associated with geophysical research with special focus on relevant climate change phenomena.

Spain

12/M64-a

Airbus Defence &...
System impacts of propulsion Passivation

Propulsion passivation is most of the time feasible for running missions, using thrusters and existing AOCS modes, whatever the number of tanks and for both monopropellant and bipropellant systems.
For monopropellant systems the propulsion passivation may be:
-Partial for tank(s) with membrane. All the hydrazine under the membrane may be depleted but the pressurant gas above the membrane cannot be depleted. The final tank pressure is close to typically 5 bars at the end of mission.

France

13-060-b

Airbus Defence &...

Pages

Filter by programme:

Filter by start year:

Filter by end year:

Filter by keywords:

Filter by contractor:

Filter by country:

Filter by application domain:

Filter by competence domain:

Filter by technology domain:

Filter by status: